The effect of second principal stress on the fatigue propagation of mode I surface crack in Al 2O 3/Al alloy composites

Abstract

Using a plate made of A2017-T6 metal matrix composites reinforced with 10 volume % and 20 volume % Al 2O 3 particles and Al alloy possesses the same composition as matrix alloy, the crack propagation rate d a/d N of a mode I surface crack by the simultaneous action of plane bending and cyclic torsion are studied. And the effects of crack tip opening stress σ top, crack opening displacement COD, biaxial stress ratio C (=second principal stress/first principal stress) and the surface roughness of crack section are examined. When stress intensity factor range ΔK is lower than the specific level, d a/d N decreases with the increase of volume fraction of Al 2O 3 in C=0 and C=−0.55. But, d a/d N of Al alloy becomes minimum in C=−1 and the effect of Al 2O 3 particles disappears. σ top rises with the increase of volume fraction of Al 2O 3 particles and the decline of C. On the other hand, COD doesn’t always rise with the decline of C. These phenomena can be explained by the residual compressive stress formed at the surface layer of the specimen by the fatigue test and the surface roughness of crack section.